RPM (R-1)RPM (R-1)
RPM (R-1)
RPM (R-1)RPM (R-1)
Operating and Installation InstructionsOperating and Installation Instructions
Operating and Installation Instructions
Operating and Installation InstructionsOperating and Installation Instructions
OI 0517911
Rev. C 9/24/97 *
You must read this manual before installing or operating the instrument. This
manual contains warranty and other information that may affect your decision
to install this product and/or the safety of your aircraft.
5/17/91
Model:Model:
Model:
Model:Model:
S/N:S/N:
S/N:
S/N:S/N:
Electronics International Inc. Electronics International Inc.
Electronics International Inc.
Electronics International Inc. Electronics International Inc.
63296 Powell Butte Hwy • Bend, OR 97701 • (541) 318-6060 • Buy-EI.com63296 Powell Butte Hwy • Bend, OR 97701 • (541) 318-6060 • Buy-EI.com
63296 Powell Butte Hwy • Bend, OR 97701 • (541) 318-6060 • Buy-EI.com
63296 Powell Butte Hwy • Bend, OR 97701 • (541) 318-6060 • Buy-EI.com63296 Powell Butte Hwy • Bend, OR 97701 • (541) 318-6060 • Buy-EI.com
®®
®
®®
Important NoticeImportant Notice
Important Notice
Important NoticeImportant Notice
***** MUST READ ********** MUST READ *****
***** MUST READ *****
***** MUST READ ********** MUST READ *****
If you think it is not important to read this manual, you're wrong!If you think it is not important to read this manual, you're wrong!
If you think it is not important to read this manual, you're wrong!
If you think it is not important to read this manual, you're wrong!If you think it is not important to read this manual, you're wrong!
This manual contains important installation information that may affectThis manual contains important installation information that may affect
This manual contains important installation information that may affect
This manual contains important installation information that may affectThis manual contains important installation information that may affect
the safety of your aircraft, delay your installation or affect the operationthe safety of your aircraft, delay your installation or affect the operation
the safety of your aircraft, delay your installation or affect the operation
the safety of your aircraft, delay your installation or affect the operationthe safety of your aircraft, delay your installation or affect the operation
of your instrument. You of your instrument. You
of your instrument. You
of your instrument. You of your instrument. You
instrument. instrument.
instrument.
instrument. instrument.
responsibility of the installer/pilot and may render the STC invalid.responsibility of the installer/pilot and may render the STC invalid.
responsibility of the installer/pilot and may render the STC invalid.
responsibility of the installer/pilot and may render the STC invalid.responsibility of the installer/pilot and may render the STC invalid.
Check that the instrument make and model marked on the side of the instrument and on the
invoice are correct before starting the installation. A R-1-6 is used on a 6-cylinder engine and a R-14 is used on a 4-cylinder engine. Also, check the invoice for proper tach time.
Check that the limit information on this instrument matches the published limits in your aircraft's
P.O.H. or Flight Manual. Also, this information may be listed in the T.C. Data Sheet for your aircraft.
Any AD's and/or STC's may set forth additional limitations on the operation of your engine. The
limit information listed in the AML is for unmodified aircraft and is intended for reference only.
the aircraft owner's and/or installer's responsibility to determine proper instrumentthe aircraft owner's and/or installer's responsibility to determine proper instrument
the aircraft owner's and/or installer's responsibility to determine proper instrument
the aircraft owner's and/or installer's responsibility to determine proper instrumentthe aircraft owner's and/or installer's responsibility to determine proper instrument
calibration and range markings using the aircraft's P.O.H.calibration and range markings using the aircraft's P.O.H.
calibration and range markings using the aircraft's P.O.H.
calibration and range markings using the aircraft's P.O.H.calibration and range markings using the aircraft's P.O.H.
Any deviation from these installation instructions is the soleAny deviation from these installation instructions is the sole
Any deviation from these installation instructions is the sole
Any deviation from these installation instructions is the soleAny deviation from these installation instructions is the sole
MustMust
Must
MustMust
read this manual prior to installing your read this manual prior to installing your
read this manual prior to installing your
read this manual prior to installing your read this manual prior to installing your
It isIt is
It is
It isIt is
On the front of this instrument you will find a red light marked with the maximum RPM information. If there are any additional red or yellow lights on this instrument, the operating range of these
lights can be found on a sticker located on the side of the instrument (see the AML at the back of this
manual to decode this information). This instrument designates any "Caution Range" with yellow
LEDs, any "Maximum and Minimum Limits" with Red LEDs and the "Safe Operating Range" with
green LEDs. The "Safe Operating Range" on this instrument is equivalent to the green "Normal
Operating Range" and any unmarked areas on a analog gauge.
Read the Warranty / AgreementRead the Warranty / Agreement
Read the Warranty / Agreement. There is information in the Warranty / Agreement that may
Read the Warranty / AgreementRead the Warranty / Agreement
alter your decision to install this product.
Agreement, do not install this productAgreement, do not install this product
Agreement, do not install this product. This product may be returned for a refund. Contact
Agreement, do not install this productAgreement, do not install this product
Electronics International inc. for details.
It is possible for any instrument to fail thereby displaying inaccurate high, low or jumpy RPM
readings. Therefore, you must be able to recognize an instrument failure and you must be proficient
in operating your aircraft safely in spite of an RPM instrument failure. If you do not have this knowledge, contact the FAA or a local flight instructor for training.
The pilot
anyone to operate the aircraft that does not know the operation of this product. Keep the Operating
Manual in the aircraft at all times.
must must
must understand the operation of this product before flying the aircraft. Do not allow
must must
If you do not accept the terms of the Warranty /If you do not accept the terms of the Warranty /
If you do not accept the terms of the Warranty /
If you do not accept the terms of the Warranty /If you do not accept the terms of the Warranty /
Rev. C 9/24/97*
ContentsContents
Contents
ContentsContents
Warranty ..............................................................................Warranty ..............................................................................
Warranty ..............................................................................
Warranty ..............................................................................Warranty ..............................................................................
Operating Instructions ............................................................Operating Instructions ............................................................
Operating Instructions ............................................................
Operating Instructions ............................................................Operating Instructions ............................................................
Instrument ---------------------------------------------------------------------------------------- 3
Analog Display ----------------------------------------------------------------------------------- 3
Digital Display ------------------------------------------------------------------------------------ 3
Mag Drop ----------------------------------------------------------------------------------------- 4
Tach Time ---------------------------------------------------------------------------------------- 4
Flight Timer and Peak RPM -------------------------------------------------------------------- 5
Installation Instructions ..........................................................Installation Instructions ..........................................................
Installation Instructions ..........................................................
Installation Instructions ..........................................................Installation Instructions ..........................................................
Important Information and Initial Check Out -------------------------------------------------- 5
Route The Circular Connector ------------------------------------------------------------------ 6
Install the Isolators ------------------------------------------------------------------------------- 6
Route the Pickup Wires ------------------------------------------------------------------------- 7
Route the Power and Ground Wires ----------------------------------------------------------- 7
Route the Backlight Wires: ---------------------------------------------------------------------- 7
Route the External Warning Control Line ----------------------------------------------------- 8
Install the Instrument in the Panel -------------------------------------------------------------- 8
Connect the Circular Connector to the Instrument ------------------------------------------- 8
Check Instrument Operation --------------------------------------------------------------------- 8
22
2
22
33
3
33
55
5
55
Wiring Diagram .....................................................................Wiring Diagram .....................................................................
Wiring Diagram .....................................................................
Wiring Diagram .....................................................................Wiring Diagram .....................................................................
R-1 Circular Connector ..........................................................R-1 Circular Connector ..........................................................
R-1 Circular Connector ..........................................................
R-1 Circular Connector ..........................................................R-1 Circular Connector ..........................................................
Specifications and Operating Features ......................................Specifications and Operating Features ......................................
Specifications and Operating Features ......................................
Specifications and Operating Features ......................................Specifications and Operating Features ......................................
STC Information ...................................................................STC Information ...................................................................
STC Information ...................................................................
STC Information ...................................................................STC Information ...................................................................
1
1010
10
1010
1111
11
1111
1212
12
1212
1313
13
1313
WW
arranty / Agreementarranty / Agreement
W
arranty / Agreement
WW
arranty / Agreementarranty / Agreement
Electronics International Inc. warrants this instrument and system components to be free from defects in
materials and workmanship for a period of one year from the user invoice date. Electronics International
Inc. will repair or replace any item under the terms of this Warranty provided the item is returned to the
factory prepaid.
1. This Warranty shall not apply to any product that has been repaired or altered by any person other than
Electronics International Inc., or that has been subjected to misuse, accident, incorrect wiring, negligence,
This warranty does notThis warranty does not
improper or unprofessional assembly or improper installation by any person.
cover any reimbursement for any person’s time for installation, removal, assembly or repair.cover any reimbursement for any person’s time for installation, removal, assembly or repair.
cover any reimbursement for any person’s time for installation, removal, assembly or repair.
cover any reimbursement for any person’s time for installation, removal, assembly or repair.cover any reimbursement for any person’s time for installation, removal, assembly or repair.
Electronics International retains the right to determine the reason or cause for warranty repair.
2. This warranty does not extend to any machine, vehicle, boat, aircraft or any other device to which the
Electronics International Inc. product may be connected, attached, interconnected or used in conjunction
with in any way.
3. The obligation assumed by Electronics International Inc. under this warranty is limited to repair, replacement or refund of the product, at the sole discretion of Electronics International Inc.
4. Electronics International Inc. is not liable for expenses incurred by the customer or installer due to
factory updates, modifications, improvements, upgrades, changes, or any other alterations to the product
that may affect the form, fit, function or operation of the product.
This warranty does not
This warranty does notThis warranty does not
5. Personal injury or property damage do to misinterpretation or lack of understanding this product is
solely the pilots responsibility. The pilot
aircraft. Do not allow anyone to operate the aircraft that does not know the operation of this product.
Keep the Operating Manual in the aircraft at all times.
6. E. I. Inc. is not responsible for shipping charges or damages incurred under this Warranty.
7. No representative is authorized to assume any other liability for Electronics International Inc. in connection with the sale of Electronics International Inc. products.
If you do not agree to and accept the terms of this warranty, you may return the productIf you do not agree to and accept the terms of this warranty, you may return the product
8.
If you do not agree to and accept the terms of this warranty, you may return the product
If you do not agree to and accept the terms of this warranty, you may return the productIf you do not agree to and accept the terms of this warranty, you may return the product
for a refund.for a refund.
for a refund.
for a refund.for a refund.
This Warranty is made only to the original user.
OTHER WARRANTIES OR OBLIGATIONS: EXPRESS OR IMPLIED. MANUFAC-OTHER WARRANTIES OR OBLIGATIONS: EXPRESS OR IMPLIED. MANUFAC-
OTHER WARRANTIES OR OBLIGATIONS: EXPRESS OR IMPLIED. MANUFAC-
OTHER WARRANTIES OR OBLIGATIONS: EXPRESS OR IMPLIED. MANUFAC-OTHER WARRANTIES OR OBLIGATIONS: EXPRESS OR IMPLIED. MANUFACTURER EXPRESSLY DISCLAIMS ALL IMPLIED WARRANTIES OF MERCHANT-TURER EXPRESSLY DISCLAIMS ALL IMPLIED WARRANTIES OF MERCHANT-
TURER EXPRESSLY DISCLAIMS ALL IMPLIED WARRANTIES OF MERCHANT-
TURER EXPRESSLY DISCLAIMS ALL IMPLIED WARRANTIES OF MERCHANT-TURER EXPRESSLY DISCLAIMS ALL IMPLIED WARRANTIES OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE. PURCHASER AGREESABILITY OR FITNESS FOR A PARTICULAR PURPOSE. PURCHASER AGREES
ABILITY OR FITNESS FOR A PARTICULAR PURPOSE. PURCHASER AGREES
ABILITY OR FITNESS FOR A PARTICULAR PURPOSE. PURCHASER AGREESABILITY OR FITNESS FOR A PARTICULAR PURPOSE. PURCHASER AGREES
THAT IN NO EVENT SHALL MANUFACTURER BE LIABLE FOR SPECIAL, INCI-THAT IN NO EVENT SHALL MANUFACTURER BE LIABLE FOR SPECIAL, INCI-
THAT IN NO EVENT SHALL MANUFACTURER BE LIABLE FOR SPECIAL, INCI-
THAT IN NO EVENT SHALL MANUFACTURER BE LIABLE FOR SPECIAL, INCI-THAT IN NO EVENT SHALL MANUFACTURER BE LIABLE FOR SPECIAL, INCIDENTAL OR CONSEQUENTIAL DAMAGES, INCLUDING LOST PROFITS OR LOSSDENTAL OR CONSEQUENTIAL DAMAGES, INCLUDING LOST PROFITS OR LOSS
DENTAL OR CONSEQUENTIAL DAMAGES, INCLUDING LOST PROFITS OR LOSS
DENTAL OR CONSEQUENTIAL DAMAGES, INCLUDING LOST PROFITS OR LOSSDENTAL OR CONSEQUENTIAL DAMAGES, INCLUDING LOST PROFITS OR LOSS
OF USE OR OTHER ECONOMIC LOSS. EXCEPT AS EXPRESSLY PROVIDEDOF USE OR OTHER ECONOMIC LOSS. EXCEPT AS EXPRESSLY PROVIDED
OF USE OR OTHER ECONOMIC LOSS. EXCEPT AS EXPRESSLY PROVIDED
OF USE OR OTHER ECONOMIC LOSS. EXCEPT AS EXPRESSLY PROVIDEDOF USE OR OTHER ECONOMIC LOSS. EXCEPT AS EXPRESSLY PROVIDED
HEREIN, MANUFACTURER DISCLAIMS ALL OTHER LIABILITY TO PURCHASERHEREIN, MANUFACTURER DISCLAIMS ALL OTHER LIABILITY TO PURCHASER
HEREIN, MANUFACTURER DISCLAIMS ALL OTHER LIABILITY TO PURCHASER
HEREIN, MANUFACTURER DISCLAIMS ALL OTHER LIABILITY TO PURCHASERHEREIN, MANUFACTURER DISCLAIMS ALL OTHER LIABILITY TO PURCHASER
OR ANY OTHER PERSON IN CONNECTION WITH THE USE OR PERFORMANCEOR ANY OTHER PERSON IN CONNECTION WITH THE USE OR PERFORMANCE
OR ANY OTHER PERSON IN CONNECTION WITH THE USE OR PERFORMANCE
OR ANY OTHER PERSON IN CONNECTION WITH THE USE OR PERFORMANCEOR ANY OTHER PERSON IN CONNECTION WITH THE USE OR PERFORMANCE
OF MANUFACTURER’S PRODUCTS, INCLUDING SPECIFICALLY LIABILITY INOF MANUFACTURER’S PRODUCTS, INCLUDING SPECIFICALLY LIABILITY IN
OF MANUFACTURER’S PRODUCTS, INCLUDING SPECIFICALLY LIABILITY IN
OF MANUFACTURER’S PRODUCTS, INCLUDING SPECIFICALLY LIABILITY INOF MANUFACTURER’S PRODUCTS, INCLUDING SPECIFICALLY LIABILITY IN
TORT.TORT.
TORT.
TORT.TORT.
must must
must understand the operation of this product before flying the
must must
THIS WARRANTY IS IN LIEU OF ALLTHIS WARRANTY IS IN LIEU OF ALL
THIS WARRANTY IS IN LIEU OF ALL
THIS WARRANTY IS IN LIEU OF ALLTHIS WARRANTY IS IN LIEU OF ALL
2
Operating InstructionsOperating Instructions
Operating Instructions
Operating InstructionsOperating Instructions
R-1R-1
R-1
R-1R-1
Instrument:Instrument:
Instrument:
Instrument:Instrument:
The R-1 is a precision RPM instrument featuring a 210 degree analog display and a full four-digit
digital display. These two displays have many advantages over conventional analog gauges as described
below.
Also, the R-1 features long-term accuracy and reliability. Since the R-1 does not incorporate any
moving parts (needles, bearings, springs, etc.) there is little to go wrong or wear out. The internal microprocessor assures accuracy and repeatability.
Analog Display:Analog Display:
Analog Display:
Analog Display:Analog Display:
The 210 degree analog display provides a quick reference of the engine’s RPM with respect to its
operating range. With a glance you can get a relative idea of how close to the maximum RPM limit the
engine is being operated and approximately how far the RPM has to increase to reach its limit. Precise
information is provided in the digital display.
0517911
An advantage of the analog display is its ability to emit a green, yellow or red light. With a quick
glance you can determine if you’re operating in a normal, caution or restricted range. Also, when you
exceed a maximum limit the red light will blink 20 times at full intensity to catch your attention and warn
you that a maximum limit has been violated. After 20 blinks the red light will stop blinking and display
continuous red so it does not distract you. The digital display will continue to display accurate RPM
readings well beyond the red line limit of the analog display.
During night operation the analog lights may be too bright. If so, turn the panel light rheostat up and
the analog lights will dim. The red (maximum limit) light will always be displayed at full intensity.
Digital Display:Digital Display:
Digital Display:
Digital Display:Digital Display:
The digital display provides RPM information in 10 RPM increments. This allows for precise setting
and monitoring of the engine RPM. Also, the digital display is excellent for monitoring trends or changes
in the engine’s performance.
For aircraft fitted with a fixed pitch prop a relative indication of an engine’s ability to produce power
can be measured by accurately monitoring the engine’s RPM during the first 5 seconds of a full power
take-off. A normal reduction in power will occur from high outside air temperatures, high altitudes and
excessively rich mixtures. Getting to know your engine’s normal take-off RPM can go a long way in
detecting engine problems early.
3
Rev. A: 6/16/92
The 10 RPM resolution of the R-1 can also help in setting the mixture control for maximum horsepower for aircraft fitted with either a fixed or variable pitch prop. This is most helpful during high altitude
climbs or take-offs. As your engine is leaned at high altitudes it may exhibit an increase in RPM. This
increase in RPM indicates an increase in power. For a variable pitch prop this will be a small change. It is
not recommended to lean an engine when operated above 75% power. Consult your engine
manufacturer’s operating procedures for proper operation.
If the digital display backlight has been permanently powered up (as recommended), the digital
display will be easier to see during low ambient light conditions and at night.
Mag Drop:Mag Drop:
Mag Drop:
Mag Drop:Mag Drop:
The mag drop feature allows you to view a change in RPM from a base line. Start by setting the
throttle to achieve normal run-up RPM. Then push both buttons on the R-1. This establishes your base
line RPM and the display will show "000". Any change in RPM (up or down from the base line) will be
displayed. RPM drops will be displayed as negative numbers (i.e.: a "- 200" display means a 200 RPM
drop from the base line). Now switch the mag to "Left" or "Right" and the RPM drop will be displayed.
Switch your mag back to "Both" and the display will return to " 000" or near " 000". Most mags will not
totally recover back to " 000". A problem (fouled plug, bad mag wire, mag problems, etc.) will show up as
excessive drop in one mag and the recover RPM (how close it returns to " 000") will be excessive. The
mag drop feature can be used to check prop governors, horsepower gain or loss during leaning and may
other engine operations.
During mag drop operation the analog display will continue to show proper engine RPM. The Mag
drop operation will automatically be canceled in 60 seconds or it may be canceled at any time by pushing
any button on the R-1.
TT
ach Time:ach Time:
T
ach Time:
TT
ach Time:ach Time:
The tach timer keeps a running total of time the engine is above 1300 RPM. The time is stored in
memory for life. There are no internal batteries and bus power is not required to keep the memory alive.
The maximum reading is 99,999.9 hours.
To display the time on the tach in thousands of hours, press the right push button marked "Tach
Time" and hold the button in. The digital display will show two digits which represent thousands of hours
on the tach.
To display the hundreds, tens, units and 1/10 hours on the tach, release the "Tach Time"To display the hundreds, tens, units and 1/10 hours on the tach, release the "Tach Time"
To display the hundreds, tens, units and 1/10 hours on the tach, release the "Tach Time"
To display the hundreds, tens, units and 1/10 hours on the tach, release the "Tach Time"To display the hundreds, tens, units and 1/10 hours on the tach, release the "Tach Time"
button for no more than two seconds and press it again and hold it in.button for no more than two seconds and press it again and hold it in.
button for no more than two seconds and press it again and hold it in. The display will show
button for no more than two seconds and press it again and hold it in.button for no more than two seconds and press it again and hold it in.
four digits with a decimal point. The digits represent hundreds, tens, units and 1/10 hours on the tach.
Each time the "Tach Time" button is pushed and held in the display will toggle between the two displays.
If the "Tach Time" button is released for more than three seconds the digital and analog displays will revert
back to RPM.
4
Rev. A: 6/16/92
Flight Timer and Peak RPM:Flight Timer and Peak RPM:
Flight Timer and Peak RPM:
Flight Timer and Peak RPM:Flight Timer and Peak RPM:
This instrument includes an automatic flight timer. When the RPM meets or exceeds 2000 RPM for
10 seconds (as would occur on takeoff), the flight timer will reset to "00.00" and start timing in one-minute
increments. The peak RPM register will also be reset to "0000". The flight timer will continue to count
until the RPM drops below 1200 RPM for 10 seconds (as would occur on the landing roll-out). At this
point the flight time and peak RPM will be stored in memory. There are no internal batteries and bus
power is not required to keep the memory alive. Your last flight time and peak RPM will always be available even if the power is turned off.
As the flight timer is counting, the maximum RPM is also being recorded. For an RPM to be recorded
as "peak" it must exceed the last recorded RPM for three seconds or longer.
To display flight time, press the push button marked "Flt
Time" and hold it in. The digital display will show your flight time in hours and minutes.
To display the highest RPM your engine reached during the flight release the "Flt Time" button for no
more than two seconds and press it again and hold it in. The digital display will show the peak RPM
reached during the flight. Each time the "Flt Time" button is pushed and held in the display will toggle
between flight time and peak RPM. If the "Flt Time" button is released for more than three seconds the
digital and analog display will revert back to RPM.
Installation InstructionsInstallation Instructions
Installation Instructions
Installation InstructionsInstallation Instructions
R-1R-1
R-1
R-1R-1
Important Information and Initial Check Out:Important Information and Initial Check Out:
Important Information and Initial Check Out:
Important Information and Initial Check Out:Important Information and Initial Check Out:
The installer and aircraft owner must read the Warranty before starting the installa-The installer and aircraft owner must read the Warranty before starting the installa-
1.
The installer and aircraft owner must read the Warranty before starting the installa-
The installer and aircraft owner must read the Warranty before starting the installa-The installer and aircraft owner must read the Warranty before starting the installa-
tion.tion.
tion. There is information in the Warranty that may alter your decision to install this instrument.
tion.tion.
you do not accept the terms of the Warranty, do not install this instrument.you do not accept the terms of the Warranty, do not install this instrument.
you do not accept the terms of the Warranty, do not install this instrument.
you do not accept the terms of the Warranty, do not install this instrument.you do not accept the terms of the Warranty, do not install this instrument.
2. If you are not an FAA Certified Aircraft Mechanic familiar with the issues of install-2. If you are not an FAA Certified Aircraft Mechanic familiar with the issues of install-
2. If you are not an FAA Certified Aircraft Mechanic familiar with the issues of install-
2. If you are not an FAA Certified Aircraft Mechanic familiar with the issues of install-2. If you are not an FAA Certified Aircraft Mechanic familiar with the issues of installing aircraft RPM instruments, ing aircraft RPM instruments,
ing aircraft RPM instruments,
ing aircraft RPM instruments, ing aircraft RPM instruments,
should use current aircraft standards and practices to install this instrument (refer toshould use current aircraft standards and practices to install this instrument (refer to
should use current aircraft standards and practices to install this instrument (refer to
should use current aircraft standards and practices to install this instrument (refer toshould use current aircraft standards and practices to install this instrument (refer to
AC 43.13).AC 43.13).
AC 43.13).
AC 43.13).AC 43.13).
Check that any necessary FAA Approvals (STC's, etc.) are available for your aircraftCheck that any necessary FAA Approvals (STC's, etc.) are available for your aircraft
3.
Check that any necessary FAA Approvals (STC's, etc.) are available for your aircraft
Check that any necessary FAA Approvals (STC's, etc.) are available for your aircraftCheck that any necessary FAA Approvals (STC's, etc.) are available for your aircraft
before starting the installation. The FAA Approved Model List (AML) is located atbefore starting the installation. The FAA Approved Model List (AML) is located at
before starting the installation. The FAA Approved Model List (AML) is located at
before starting the installation. The FAA Approved Model List (AML) is located atbefore starting the installation. The FAA Approved Model List (AML) is located at
the back of this manual. the back of this manual.
the back of this manual.
the back of this manual. the back of this manual.
lation.lation.
lation.
lation.lation.
4. Before starting installation, read the entire Installation Instructions and resolve any installation,
operating and performance issues you may have. This may eliminate any delays once the installation is started. If the tach cable is removed, a RPM cap is available to cover the port (see price
sheet).
Do Not attempt to install this instrument.Do Not attempt to install this instrument.
Do Not attempt to install this instrument.
Do Not attempt to install this instrument.Do Not attempt to install this instrument.
Resolve any issues you may have before starting the instal-Resolve any issues you may have before starting the instal-
Resolve any issues you may have before starting the instal-
Resolve any issues you may have before starting the instal-Resolve any issues you may have before starting the instal-
The installer The installer
The installer
The installer The installer
IfIf
If
IfIf
5
Rev. C 9/24/97
5. Check that the instrument make and model marked on the side of the instrument and on the invoice
are correct before starting the installation. A R-1-6 is used on a 6-cylinder engine and a R-1-4 is
used on a 4-cylinder engine. The R-1-?S1 or R-1-?S2 is to be used on a Lasar ignition system (or
any system with a tach out). Also, check the invoice for proper tach time.
6. Check that the limit information on this instrument matches the published limits in your aircraft's
P.O.H. or Flight Manual. Also, this information may be listed in the T.C. Data Sheet for your
aircraft. Any AD's and/or STC's may set forth additional limitations on the operation of your
engine. The limit information listed in the AML is for unmodified aircraft and is intended for
It is the aircraft owner's and/or installer's responsibility to determineIt is the aircraft owner's and/or installer's responsibility to determine
reference only.
proper instrument calibration and range markings for your aircraft.proper instrument calibration and range markings for your aircraft.
proper instrument calibration and range markings for your aircraft.
proper instrument calibration and range markings for your aircraft.proper instrument calibration and range markings for your aircraft.
On the front of this instrument you will find a red light marked with the maximum RPM informa-
tion. If there are any additional red or yellow lights on this instrument, the operating range of these
lights can be found on a sticker located on the side of the instrument (see the AML at the back of
this manual to decode this information). This instrument designates any "Caution Range" with
yellow LEDs, any "Maximum and Minimum Limits" with Red LEDs and the "Safe Operating
Range" with green LEDs. The "Safe Operating Range" on this instrument is equivalent to the green
"Normal Operating Range" and any unmarked areas on a analog gauge.
Do not attempt to remove or replace the limit stickers on this instrument. If the RPM limits for your
engine do not match those which are marked on this instrument send this unit back to Electronics
International Inc. for re-calibration.
that is not properly calibrated for your aircraft.that is not properly calibrated for your aircraft.
that is not properly calibrated for your aircraft.
that is not properly calibrated for your aircraft.that is not properly calibrated for your aircraft.
It is the aircraft owner's and/or installer's responsibility to determine
It is the aircraft owner's and/or installer's responsibility to determineIt is the aircraft owner's and/or installer's responsibility to determine
DO NOT install or use a primary engine instrumentDO NOT install or use a primary engine instrument
DO NOT install or use a primary engine instrument
DO NOT install or use a primary engine instrumentDO NOT install or use a primary engine instrument
7. Before starting the installation make sure the unit will fit in the location you intend to install it
without obstructing the operation of any controls.
8. If this instrument is to replace an existing unit in the aircraft, it is the installer's responsibility to
move or replace any existing instruments or components in accordance with FAA approved methods and procedures. The following Installation Instructions do not cover moving or the removal of
any existing instruments or components.
Route The Circular Connector:Route The Circular Connector:
Route The Circular Connector:
Route The Circular Connector:Route The Circular Connector:
Starting from under the instrument panel, route the circular connector end of the wire harness up to
the instrument mounting location. (See the wiring diagram at the back of this manual). Place the circular
connector about 8 inches back from the panel. Tie wrap the harness in place approximately 1 foot back
from the circular connector. This will allow the harness to be flexible and accommodate varying lengths in
instrument wires.
Install the Isolators:Install the Isolators:
Install the Isolators:
Install the Isolators:Install the Isolators:
On the back of the mag switch will be a number of lugs. Locate the two lugs connected to the left
and right mag leads (P leads). Connect the two isolators supplied with the kit to these lugs (see wiring
diagram). When installing these isolators do not remove the existing mag leads (P leads).
Be sure these wires do not obstruct the freedom of travel of any controls.Be sure these wires do not obstruct the freedom of travel of any controls.
Be sure these wires do not obstruct the freedom of travel of any controls.
Be sure these wires do not obstruct the freedom of travel of any controls.Be sure these wires do not obstruct the freedom of travel of any controls.
These isola-These isola-
These isola-
These isola-These isola-
6
Rev. B: 6/3/94
tors should not be changed, lengthened or altered in any way.tors should not be changed, lengthened or altered in any way.
tors should not be changed, lengthened or altered in any way. There is another set of isolators in
tors should not be changed, lengthened or altered in any way.tors should not be changed, lengthened or altered in any way.
the instrument. These isolators insure safe operation while providing an easy and simple installation free of
mechanical cables and pickups.
not interfering or shorting to any other terminals on the mag switch.not interfering or shorting to any other terminals on the mag switch.
not interfering or shorting to any other terminals on the mag switch.
not interfering or shorting to any other terminals on the mag switch.not interfering or shorting to any other terminals on the mag switch.
Route the Pickup Wires:Route the Pickup Wires:
Route the Pickup Wires:
Route the Pickup Wires:Route the Pickup Wires:
Route the orange wire and the brown wire from the wire harness to the isolators. Cut to length and
install a male slip-on connector on each wire. Double over the stripped wire before inserting it into the
male connector. Double crimp the connector making sure the crimping tool closes completely. Now mate
the orange wire and the brown wire to the female connectors on the isolators. Either wire may connect to
either isolator. Be sure the connectors mate properly. If the tab in the male connector gets bent, it can
wedge itself between the red nylon and the female metal receptacle. This can result in an intermittent
connection after about a month or more. If the connectors are removed several times, the female connector
can become loose. If this happens, use a pair of needle nose pliers and tighten the metal receptacle inside
the female connector.
controls.controls.
controls.
controls.controls.
Route the Power and Ground Wires:Route the Power and Ground Wires:
Route the Power and Ground Wires:
Route the Power and Ground Wires:Route the Power and Ground Wires:
Tie wrap these wires so they do not obstruct the freedom of travel of anyTie wrap these wires so they do not obstruct the freedom of travel of any
Tie wrap these wires so they do not obstruct the freedom of travel of any
Tie wrap these wires so they do not obstruct the freedom of travel of anyTie wrap these wires so they do not obstruct the freedom of travel of any
Make sure the mag lead screws are tight and the connectors areMake sure the mag lead screws are tight and the connectors are
Make sure the mag lead screws are tight and the connectors are
Make sure the mag lead screws are tight and the connectors areMake sure the mag lead screws are tight and the connectors are
Route the red wire in the wire harness to the aircraft’s 12 or 24 volt main or emergency bus as applicable via an independent circuit breaker (five amps or less). An alternate method would be to route the red
lead to the bus via a one amp in-line fuse. With this method a spare fuse should be kept in the aircraft.
Route the black wire in the wire harness to a good ground .
obstruct the freedom of travel of any controls.obstruct the freedom of travel of any controls.
obstruct the freedom of travel of any controls.
obstruct the freedom of travel of any controls.obstruct the freedom of travel of any controls.
Route the Backlight Wires:Route the Backlight Wires:
Route the Backlight Wires:
Route the Backlight Wires:Route the Backlight Wires:
Connect the backlight wires as follows:
1. It is recommended to permanently power up the digital display backlight.
a) For a 12-volt system connect the white/brown wire to the instrument red power lead.
Connect the white/red wire to ground (see Wiring Diagram).
b) For a 24-volt system leave the white/brown open and connect the white/red wire to the
instrument red power lead (see Wiring Diagram).
2. Connect the white/orange wire to the panel light rheostat. This wire will dim the analog LED’s
for night operation when the panel lights are turned on. If this line is left open, the analog LED's
will remain at full intensity at all times. Also, if the voltage on this line drops below 11.5 volts,
the analog LED's will be displayed at full intensity.
struct the freedom of travel of any controls.struct the freedom of travel of any controls.
struct the freedom of travel of any controls. Note: This line may be connected to the CP-1
struct the freedom of travel of any controls.struct the freedom of travel of any controls.
Intensity Control Pot (see price sheet.
Tie wrap these wires so they do notTie wrap these wires so they do not
Tie wrap these wires so they do not
Tie wrap these wires so they do notTie wrap these wires so they do not
Tie wrap all wires so they do not ob-Tie wrap all wires so they do not ob-
Tie wrap all wires so they do not ob-
Tie wrap all wires so they do not ob-Tie wrap all wires so they do not ob-
7
Rev. C 9/24/
97
Route the External WRoute the External W
Route the External W
Route the External WRoute the External W
The white/yellow wire can be connected to an external light (AL-1), buzzer (ATG-1), voice annunciator (AV-17), a relay, etc. This wire grounds when the red warning light is on. The current in this line must
be limited to 1/10 of an amp maximum. Exceeding this limit will damage the unit. If this feature is not
used leave this line open.
controls.controls.
controls.
controls.controls.
arning Control Line:arning Control Line:
arning Control Line:
arning Control Line:arning Control Line:
Tie wrap this wire so it does not obstruct the freedom of travel of anyTie wrap this wire so it does not obstruct the freedom of travel of any
Tie wrap this wire so it does not obstruct the freedom of travel of any
Tie wrap this wire so it does not obstruct the freedom of travel of anyTie wrap this wire so it does not obstruct the freedom of travel of any
Install the Instrument in the PInstall the Instrument in the P
Install the Instrument in the P
Install the Instrument in the PInstall the Instrument in the P
Install the instrument from behind the instrument panel using 6 x 32 screws. These screws should not
be any longer than 1/2".
Connect the Circular Connector to the Instrument:Connect the Circular Connector to the Instrument:
Connect the Circular Connector to the Instrument:
Connect the Circular Connector to the Instrument:Connect the Circular Connector to the Instrument:
1. Push the two mating connectors together and twist them until they snap into position.
2. Turn the locking ring on the instrument connector clockwise (1 1/2 turns) until it locks into position.
Check Instrument Operation:Check Instrument Operation:
Check Instrument Operation:
Check Instrument Operation:Check Instrument Operation:
To check instrument operation perform the follows:
1. Turn the master switch on and verify that the instrument sequences through all the analog lights and
reads "8888" on the digital display for 3 seconds or less and then switches to "0000." A problem at
this step could be caused by poor connections on the red and/or black leads.
anel:anel:
anel:
anel:anel:
2. Check the digital display backlight. With high or medium ambient light it is hard to see the digital
display backlight (it is only required during low ambient light conditions but should be on all the
time).
3. Start the aircraft engine and allow it to idle with the mag switch on "Both." The digital and analog
display should be reading properly. An engine’s RPM will fluctuate 10 to 20 RPM at low idle. A
problem at this step could be caused by a poor or improper connection on the brown or orange mag
wires. To troubleshoot, connect the brown mag wire to the mag (through an isolator), leave the
orange mag wire disconnected and look for proper operation with the engine at a stable idle RPM.
Then connect the orange mag wire to the mag (through an isolator) and leave the brown mag wire
disconnected. Look for proper operation with the engine at a stable idle RPM.
4. With all wires connected and the engine at idle select "Left" on the mag switch. Check the analog
and digital display for proper operation. A large drop in the RPM for one second is normal. The
microprocessor is switching to the other mag. Do this same test for the right mag. A problem at
this step could be caused by a poor or improper connection on the brown or orange pickup cables.
To troubleshoot see step 3 above.
8
Rev. C 9/24/97
5. Bring the engine RPM up to 1500 and look for proper operation. A jumpy high RPM reading at this
step may be cause by a higher than normal voltage output from a Bendix Mag. If this is the case,
install the Bendix Isolators supplied in your R-1 package.
6. Check that the screws on the mag switch have been properly tightened and the connectors are not
interfering or shorting to any other terminals on the mag switch.
9
RPM (R-1)RPM (R-1)
RPM (R-1)
RPM (R-1)RPM (R-1)
Wiring Diagram Wiring Diagram
Wiring Diagram
Wiring Diagram Wiring Diagram
WD 0311911
Do not use screws longer
than 1/2" (4 ea.).
Circular Connector
Red
Black
White/Brwn
White/Red
Wire Harness
White/Orng
White/Yel
Brown
Orange
Power Lead, connects to 12 or 24 Volt Bus via one amp fuse.
Ground Lead, connects to Ground.
12V Backlight Control Line, connects to Red Power Lead for a 12V system via
the power fuse. 12 volts turns on the digital display backlight.
24V Backlight Control Line, connects to Red Power Lead for a 24V system via
the power fuse.
Analog LED Lighting Control Line, connects to Panel Light Rheostat. 12/24
volts dims the analog LEDs.
External Warning Control Line. Can be connected to a relay to control an
external light, buzzer, etc. Grounds when Red Warning Light is on. Current
must be limited to 1/10 amp maximum.
Connect to ground for 12 Volt System.Connect to ground for 12 Volt System.
Connect to ground for 12 Volt System.
Connect to ground for 12 Volt System.Connect to ground for 12 Volt System.
Isolator
Isolator
To Left or Right Mag Lead.
To the Other Mag Lead.
10
Rev. A: 6/16/92
R-1 Circular ConnectorR-1 Circular Connector
R-1 Circular Connector
R-1 Circular ConnectorR-1 Circular Connector
Connecting Cable Harness, Back View (wire side)
W/
3
Yel
W/
6
Org
9
Blk
W/
Red
Brwn
Red
W/
Brn
Orng
1
4
7
Note: See Wiring Diagram for
hook up information.
11
Rev. A: 6/16/92
Specifications and Operating FeaturesSpecifications and Operating Features
Specifications and Operating Features
Specifications and Operating FeaturesSpecifications and Operating Features
S0520911
Model:
R-1 (RPM Instrument)
Case Dimensions:
2.5" x 2.5" x 3.65" depth, 2 1/4" Bezel.
Weight:
10 Oz.
Environmental:
Meets TSO C49a.
Power Requirements:
7.5 to 30 Volts, 1/10 Amp.
Analog Display:
17 High Intensity Light Emitting Diodes (LEDs) in a 210 degree arc with Intensity Control Line
available for dimming. Sequential flash test on power up. Microprocessor eliminates LED hunting
(flicker).
Red LEDs:
If the Analog Display goes from a Green LED or Yellow LED to a Red LED, the Red LED will blink
20 times then go solid red. The Red Max Limit LED is always displayed at full intensity.
Digital Display:
LCD (viewable in direct sunlight), with 12 and 24 volt backlight control wires for night operation.
Readings below 300 RPM will be displayed as "0000". Display will read "8888" on power up.
Accuracy:
1% in accordance with TSO C49a.
Resolution:
10 RPM.
Max Digital Range:
4300 RPM.
Update Time:
3 times per second.
12
Rev. A: 6/16/92
Signal Pickup:
Connects to Left and Right Mag Leads through isolators. Safety insured by additional in-line isolators
located in the unit. Instrument will operate on Mags, CDIs and automotive ignition systems. No
cables or mechanical connections required.
Tach Time:
Keeps a running total time for RPM readings at or above 1300 RPM. Time is stored in memory for
life. There are no internal batteries and power is not required to keep memory alive. Maximum
reading is 99,999.9 hours. Displayed in .1 hour increments.
Automatic Flight Time:
Resets to "00.00" and starts timing when RPM reading reaches or exceeds 2000 for 10 seconds. Stops
Flight Timer and holds reading in memory when RPM drops below 1200 RPM for 10 seconds. Maximum reading is 99.59 (99 hours and 59 minutes). Displayed in 1 minute increments.
Peak RPM:
Operates in conjunction with the Automatic Flight Timer. Stores the highest RPM for the flight. For
an RPM to be recorded as "peak" it must exceed the last recorded peak RPM for 3 seconds or longer.
External Warning Control Line:
Grounds when any Red Warning Light is on or blinking. Current should be limited to 2/10 amp.
STC InformationSTC Information
STC Information
STC InformationSTC Information
The R-1 is TSO'd, STC'd and PMA'd as a primary instrument. If you have any question on which
aircraft are included on our Approved Model List (AML), please call our factory.
13
Rev. A: 6/16/92
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